Limitations Flashcards
1
Q
Maximum Cargo Compartment Loads
E175
A
Forward: 3307
Aft: 2535
2
Q
Maximum Cargo Compartment Loads
E170
A
Forward: 3020
Aft: 2271
3
Q
Max tailwind component:
A
10 knots
4
Q
Max Runway Slope
A
+/-2%
5
Q
Acceleration Load Limits
Flaps Up
A
-1.0G to +2.5G
6
Q
Acceleration Load Limits
Flaps 1, 2, 3, 4, 5, and full
A
0.0G to +2.0G
7
Q
Max Operating Altitude
A
FL410
8
Q
Max Takeoff and Landing Altitude
A
8,000
9
Q
Max Ambient Air Temperature for Takeoff and Landing
A
52°C
10
Q
Max Flap Extension Altitude
A
FL200
11
Q
Max Operating Latitude
A
78°N to 78°S
12
Q
Min Ambient Temperature for Takeoff and Landing
A
-40°C
13
Q
Maximum Landing Gear Extended Speed
A
250 KIAs
14
Q
Maximum Gear Retraction Speed
A
250 KIAs
15
Q
Maximum Gear Extended Speed
A
250 KIAs
16
Q
VFE Flaps 1
A
230 KIAs
17
Q
VFE Flaps 2
A
215 KIAs
18
Q
VFE Flaps 3
A
200 KIAs
19
Q
VFE Flaps 4
A
180 KIAs
20
Q
VFE Flaps 5
A
180 KIAs
21
Q
VFE Flaps Full
A
165 KIAs
22
Q
Design Maneuvering Speed
A
240 KIAs
23
Q
Definition of Icing Conditions?
A
10°C or below; and
-Visible moisture in any form is present;
or
When operating on contaminated surfaces.
24
Q
Fuel Quantity per Tank
A
10,393 lbs
25
Unusable Fuel Quantity per Tank
75 lbs
26
Aircraft Maximum Fuel Capacity (Usable + unusable)
20,936 lbs
27
Maximum Windshield Wiper Operation Speed
250 KIAs
28
Fuel Imbalance
790 lbs
29
Crossfeed Limitations
XFEED Selector must be set to OFF during takeoff and landing.
30
Minimum Fuel Tank Temperature
-37°C
31
Brake Cooling Limitation
Do not take off with amber brake temperature indicators.
32
Landing Gear Retraction (Activation of landing gear downlock release button)
Prohibited for all takeoffs except when obstacle clearance is required.
33
What is prohibited regarding flaps use?
Holding in Icing conditions with flaps extended
Using Flaps 4 during approach and landing
Enroute use of flaps
34
Thrust Reverser Limitations
Ground use only
Do not attempt go around after thrust reverser deployment
Power back operations prohibited
Must be stowed below 60 knots
Once deployed, do not move thrust reversers into the forward thrust range until the REV is shown green on EICAS
35
When must thrust reversers be stowed?
Below 60 knots.
36
When are TAS, TAT and SAT valid?
Above 60 knots
37
When are LOC back courses N/A?
Using IESS
38
What equipment is required to operate in RVSM airspace?
2 RVSM Compliant Air Data systems
1 Autopilot ENGAGED with altitude holding mode operative
1 altitude alerter
1 Transponder
39
What is the maximum allowable altitude difference between PFD 1 and PFD 2 for RVSM operations?
200 ft
40
What is the maximum altimeter difference allowed between altimeter indications on the ground?
75 feet
41
Minimum Autopilot Engagement Height
400 ft AGL
42
Minimum Autopilot Use Height: ILS Approach
-50 ft
43
Minimum Autopilot Use Height: Non-Precision Approach
MDA (DA)
44
Minimum Autopilot Use Height: Visual Approach
400 ft AGL (C)
45
Maximum Crosswind Component for Cat II Approach
12 knots
46
CAT II Required Equipment
- 2 Intertial Reference Systems
- 2 ADS
- 2 PFDs
- 1 EGPWS
- SPOILER FAULT message not presented
- 2 VOR/ILS Nav Systems
- 1 VHF/COMM System
- Autothrottles
- Rudder in normal mode
- 1 Radar Altimeter
- 2 Flight Director Systems
- 1 Autopilot with 1 operating channel
- Windshield Wipers
- 1 CAT II Engagement Logic
47
What flaps setting is required for CAT II Approach?
Flaps 5
48
Minimum Use Height for CAT II approach
50' AGL
49
Engine N1 Maximum
99.5%
50
Engine N2 Minimum
58.5%
51
Engine N2 Maximum
99.4%
52
ITT Start Maximum
855°
53
ITT Max Continuous
960°C
54
Oil Pressure Operating Range
25-95 PSI
55
Oil Temperature Continuous
155°C
56
Oil Temperature Transient
163°C (Time limited to 15 minutes above 155°C.
57
How long is the engine warm up/ cool down periods?
2 minutes
58
When is reduced thrust takeoff not authorized?
Runway contaminated with standing water, slush, snow or ice
Windshear present or suspected
Performance mandates NO FLEX
59
Engine Starter Duty Cycle Limits
Attempts 1-2
Ground and Inflight
Ground: 90 Seconds ON/ 10 seconds OFF
| In flight: 120 Seconds ON/ 10 seconds OFF
60
Engine Starter Duty Cycle Limits
Attempts 3-5
Ground and Inflight
Ground: 90 seconds ON/ 5 minutes OFF
Inflight: 120 seconds on/ 5 minutes OFF
61
Engine Starter Dry Motoring Duty Cycle Limits
1st Attempt
Ground and Inflight
90 seconds ON/ 5 minutes OFF
62
Engine Starter Dry Motoring Duty Cycle Limits
Attempts 2-5
Ground and Inflight
30 seconds ON/ 5 minutes OFF
63
When is single engine taxi not authorized?
Braking Action Less than Good
| RVR <1200
64
APU Start Min Temperature
-54°C
65
APU Max Start Altitude
30,000 feet
66
APU Max Operating Altitude
33,000 feet
67
APU Bleed Max Altitude
15,000 feet
68
APU Max Altitude Engine Start
21,000 feet
69
APU Max Rotor Speed
108%
70
APU Continuous Max Temp
717°C
71
APU Max Start Temp
1032°C
72
Max Differential Pressure
8.4 psi
73
Max Differential Overpressure
8.8 psi
74
Max altitude for single pack operation
31,000
75
Max differential negative Pressure
-.5 psi
76
Maximum Differential Overpressure for Takeoff and Landing
.2 psi
77
Maximum Recommended Crosswind
38 knots
78
Maximum Speed to Open the Direct Vision Window
160 knots
79
Maximum Tire Ground Speed
195 knots
80
Maximum Recommended Crosswind
RCC 6
38 Knots
81
Maximum Recommended Crosswind
RCC 5 Good
31 knots
82
Maximum Recommended Crosswind
RCC 4 Good to Medium
20 knots
83
Maximum Recommended Crosswind
RCC 3 Medium
15 knots
84
Maximum Recommended Crosswind
RCC 2 Medium to Poor
12
85
Maximum Recommended Crosswind
RCC 1 Poor
8 knots
86
Max Ramp Weight
E175: 85,870
E170: 82,364
87
Maximum Takeoff Weight
E175: 85,517
E170: 82,011
88
Max Landing Weight
E175: 74,957
E170: 72,310
89
Max Zero Fuel Weight
E175: 69,886
E170: 65,256
